Supersonic Inlets

51 books
Analysis of inlet-compressor acoustic interactions using coupled CFD codesUnknown Author

Analysis of inlet-compressor acoustic interactions using coupled CFD codes

Unknown Author

1998No page data
Analysis of inlet-compressor acoustic interactions using coupled CFD codesUnknown Author

Analysis of inlet-compressor acoustic interactions using coupled CFD codes

Unknown Author

1998No page data
Study of compressible flow through a rectangular-to-semiannular transition ductUnknown Author

Study of compressible flow through a rectangular-to-semiannular transition duct

Unknown Author

1995No page data
An investigation of bleed configurations and their effect on shock wave/boundary layer interactionsA. Hamed

An investigation of bleed configurations and their effect on shock wave/boundary layer interactions

A. Hamed

1995No page data
Joint US/Russia TU-144 engine ground testsUnknown Author

Joint US/Russia TU-144 engine ground tests

Unknown Author

1997No page data
Joint US/Russia TU-144 engine ground testsUnknown Author

Joint US/Russia TU-144 engine ground tests

Unknown Author

1997No page data
Joint US/Russia TU-144 engine ground testsUnknown Author

Joint US/Russia TU-144 engine ground tests

Unknown Author

1997No page data
An experimental device for generating high frequency perturbations in supersonic wind tunnelsKevin J. Melcher

An experimental device for generating high frequency perturbations in supersonic wind tunnels

Kevin J. Melcher

1996No page data
Numerical simulation of supersonic and hypersonic inlet flow fieldsD. Scott McRae

Numerical simulation of supersonic and hypersonic inlet flow fields

D. Scott McRae

1995No page data
A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow fieldScott Douglas Holland

A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field

Scott Douglas Holland

1991No page data
Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D codeKamlesh Kapoor

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Kamlesh Kapoor

1994No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott D. Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott D. Holland

1994No page data
The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transportDavid Soreide

The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport

David Soreide

1999No page data
Validation of WIND for a series of inlet flowsJohn W. Slater

Validation of WIND for a series of inlet flows

John W. Slater

2002No page data
Numerical simulation of supersonic flow using a new analytical bleed boundary conditionG. J. Harloff

Numerical simulation of supersonic flow using a new analytical bleed boundary condition

G. J. Harloff

1995No page data
Mach 10 computational study of a three-dimensional scramjet inlet flow fieldScott Douglas Holland

Mach 10 computational study of a three-dimensional scramjet inlet flow field

Scott Douglas Holland

1995No page data
A preliminary design study of supersonic through-flow fan inletsPaul J. Barnhart

A preliminary design study of supersonic through-flow fan inlets

Paul J. Barnhart

1988No page data
A method for generating reduced order linear models of supersonic inletsAmy Chicatelli

A method for generating reduced order linear models of supersonic inlets

Amy Chicatelli

1997No page data
Computation of multi-dimensional viscous supersonic jet flowY. N. Kim
⏱ 2h 4m

Computation of multi-dimensional viscous supersonic jet flow

Y. N. Kim

1986124 pp.
A method for generating reduced-order linear models of multidimensional supersonic inletsAmy Chicatelli

A method for generating reduced-order linear models of multidimensional supersonic inlets

Amy Chicatelli

1998No page data
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